Method of fabricating a spherical cavitation chamber

ABSTRACT

A method of fabricating a spherical cavitation chamber is provided. Depending upon the chamber&#39;s composition and wall thickness, chambers fabricated with the disclosed techniques can be used with either low or high pressure systems. During chamber fabrication, initially two spherical half portions are fabricated and then the two half portions are joined together to form the desired cavitation chamber. During the fabrication of each chamber half, the interior spherical surface is completed first and then the outer spherical surface. Prior to joining the two spherical cavitation chamber halves, the surfaces to be mated are finished, preferably to a surface flatness of at least ±0.01 inches. Brazing is used to join the chamber halves together. The brazing material is preferably in the form of a ring-shaped sheet with outside and inside diameters of approximately the same size as the cavitation sphere&#39;s outside and inside diameters. Preferably the brazing operation is performed under vacuum conditions. During brazing, preferably force is applied to the two half spheres in order to compress the brazing material and achieve a strong bond. In order to insure that the inner surface of the completed cavitation chamber is relatively smooth, means for aligning the two half spheres during brazing is required, the means being either integral or external to the half spheres.

FIELD OF THE INVENTION

The present invention relates generally to sonoluminescence and, more particularly, to a method of fabricating a sonoluminescence cavitation chamber.

BACKGROUND OF THE INVENTION

Sonoluminescence is a well-known phenomena discovered in the 1930's in which light is generated when a liquid is cavitated. Although a variety of techniques for cavitating the liquid are known (e.g., spark discharge, laser pulse, flowing the liquid through a Venturi tube), one of the most common techniques is through the application of high intensity sound waves.

In essence, the cavitation process consists of three stages; bubble formation, growth and subsequent collapse. The bubble or bubbles cavitated during this process absorb the applied energy, for example sound energy, and then release the energy in the form of light emission during an extremely brief period of time. The intensity of the generated light depends on a variety of factors including the physical properties of the liquid (e.g., density, surface tension, vapor pressure, chemical structure, temperature, hydrostatic pressure, etc.) and the applied energy (e.g., sound wave amplitude, sound wave frequency, etc.).

Although it is generally recognized that during the collapse of a cavitating bubble extremely high temperature plasmas are developed, leading to the observed sonoluminescence effect, many aspects of the phenomena have not yet been characterized. As such, the phenomena is at the heart of a considerable amount of research as scientists attempt to not only completely characterize the phenomena (e.g., effects of pressure on the cavitating medium), but also its many applications (e.g., sonochemistry, chemical detoxification, ultrasonic cleaning, etc.). A by-product of this research have been several patents claiming various aspects of the process. One such patent, U.S. Pat. No. 4,333,796, discloses a cavitation chamber that is generally cylindrical although the inventors note that other shapes, such as spherical, can also be used. It is further disclosed that the chamber is comprised of a refractory metal such as tungsten, titanium, molybdenum, rhenium or some alloy thereof. U.S. Pat. No. 4,333,796 does not disclose any techniques for fabricating the chamber. Similarly U.S. Pat. No. 4,563,341, a continuation-in-part of U.S. Pat. No. 4,333,796, does not disclose fabrication techniques for use with the disclosed cylindrical chamber. Rather, the patent simply discloses the preferred materials for the chamber walls and chamber linings and the preferred mounting locations for an array of acoustic horns.

U.S. Pat. No. 5,659,173 discloses a sonoluminescence system that uses a transparent spherical flask. The spherical flask is not described in detail, although the specification discloses that flasks of Pyrex®, Kontes®, and glass were used with sizes ranging from 10 milliliters to 5 liters.

U.S. Pat. No. 5,858,104 discloses a shock wave chamber partially filled with a liquid. The remaining portion of the chamber is filled with gas which can be pressurized by a connected pressure source. Acoustic transducers mounted in the sidewalls of the chamber are used to position an object within the chamber. Another transducer mounted in the chamber wall delivers a compressional acoustic shock wave into the liquid. A flexible membrane separating the liquid from the gas reflects the compressional shock wave as a dilation wave focused on the location of the object about which a bubble is formed. The shape, composition and fabrication of the shock wave chamber is not disclosed.

U.S. Pat. No. 6,361,747 discloses an acoustic cavitation reactor. The reactor chamber is comprised of a flexible tube through which the liquid to be treated circulates. The acoustic transducers are radially distributed around the tube. As disclosed, the reactor tube may be comprised of a non-resonant material such as a resistant polymeric material (e.g., TFE, PTFE), with or without reinforcement (e.g., fiberglass, graphite fibers, mica).

Although not in the field of sonoluminescence, U.S. Pat. No. 4,448,743 discloses a confinement chamber for use with an ultra-high temperature steady-state plasma. Although the plasma is referred to as a “plasmasphere”, the specification is unclear as to whether the confinement chamber is spherical or cylindrical in nature. Furthermore a method of fabricating the disclosed chamber is not provided. Rather, the patent simply discloses the design requirements for such a chamber. For example, in describing the requirements for an isochoric heating system, the patent discloses that the vessel should be capable of containing a pressure that is slowly increased from 1.82 atmospheres to 22.1 atmospheres and be fitted with infrared and far-infrared windows as well as a down-draft vertical hydrogen jet.

Although a variety of sonoluminescence systems have been designed, typically these systems are intended for low pressure research and therefore are comprised of glass or similar material. Those designed for higher pressures are usually cylindrically shaped. Those researchers who have suggested the use of spherical chambers have not disclosed how to fabricate such a chamber to enable it to handle high pressure. Accordingly, what is needed is a method of fabricating a spherical cavitation chamber that can be used for high pressure sonoluminescence. The present invention provides such a method.

SUMMARY OF THE INVENTION

The present invention provides a method of fabricating a spherical cavitation chamber for sonoluminescence. Depending upon both the chamber's composition and wall thickness, chambers fabricated with the disclosed techniques can be used with either low or high pressure systems.

According to the invention, chamber half portions are first fabricated and then the two half portions are joined together to form the desired cavitation chamber. According to one embodiment, during the fabrication of each chamber half, the interior surface, the mating surface and a portion of the exterior surface are fabricated while the piece of stock is mounted within a first lathe chuck. The stock piece is then un-mounted, reversed, and mounted within a second lathe chuck. The second lathe chuck may be the same as the first lathe chuck, or the second lathe chuck may have jaws with holding surfaces which match the curvature of the exterior surface of the chamber half. Once mounted within the second lathe chuck, the remaining portion of the exterior surface is turned. According to a second embodiment, during the fabrication of each chamber half the interior spherical surface is completed first along with a cylindrical portion. The stock piece is then un-mounted, reversed, and remounted prior to turning the exterior spherical surface. The cylindrical portion is then removed and the mating surface finished.

According to another aspect of the invention, joining the half spherical portions together is accomplished with a brazing material suitable for use with the material comprising the half spheres. The brazing material is preferably in the form of a ring-shaped sheet with outside and inside diameters of approximately the same size as the cavitation sphere's outside and inside diameters. The two half spheres, with interposed brazing material, are then placed in a suitable chamber which is evacuated and heated to a temperature above the melting temperature of the brazing material. During the brazing operation, preferably force is applied to the two spherical cavitation chamber halves in order to compress the brazing material and achieve a strong braze. In order to insure that the inner surface of the completed cavitation chamber is relatively smooth, means for aligning the two half spheres during brazing is required. The means can be integral to the half spheres, for example alignment pins/holes. Alternately the means can be external to the half sphere, for example an alignment jig.

In at least one embodiment of the invention, the cavitation chamber is fabricated from stainless steel and the brazing material is comprised of nickel, chromium, silicon and boron. A force of approximately 1000 lbs is used during the brazing operation, the brazing temperature in the range of 1550° to 1650° F.

In at least one embodiment of the invention, after the cavitation chamber is finished, at least one acoustic transducer is coupled to the chamber in order to drive sonoluminescence within the chamber.

A further understanding of the nature and advantages of the present invention may be realized by reference to the remaining portions of the specification and the drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is an illustration of a spherical sonoluminescence cavitation chamber fabricated in accordance with the invention;

FIG. 2 is a cross-sectional view of a spherical cavitation chamber fabricated in accordance with the invention;

FIG. 3 illustrates the first step of chamber fabrication in which a piece of stock material is mounted within a lathe chuck;

FIG. 4 illustrates the step in which the inside surface of a spherical chamber half is fabricated;

FIG. 5 illustrates the step in which a portion of the outside surface of the chamber half of FIG. 4 is fabricated;

FIG. 6 is a cross-sectional view of a chuck assembly in which the jaws are shaped to match the curvature of the outside surface of the chamber half shown in FIG. 5;

FIG. 7 is an end-view of the chuck assembly of FIG. 6;

FIG. 8 illustrates the chamber half of FIG. 5 mounted within the chuck assembly of FIGS. 6 and 7;

FIG. 9 illustrates the step in which the last remaining portion of the spherical chamber half of FIG. 4 is fabricated;

FIG. 10 illustrates the mounting of a larger stock piece in the lathe chuck assembly in accordance with a second embodiment of the invention;

FIG. 11 illustrates the step in which the inside surface of a spherical chamber half and a cylindrical portion are fabricated in accordance with the second embodiment;

FIG. 12 illustrates the step of reversing the mounting configuration of the spherical chamber half in accordance with the second embodiment;

FIG. 13 illustrates the step in which the outside surface of the spherical chamber half of FIG. 11 is fabricated in accordance with the second embodiment;

FIG. 14 illustrates a pair of spherical chamber halves with a brazing material interposed between the surfaces to be joined;

FIG. 15 is a frontal view of the ring of brazing material;

FIG. 16 illustrates the step of joining two half spheres, the half spheres including alignment means;

FIG. 17 illustrates a preferred brazing jig;

FIG. 18 is a frontal view of a portion of the brazing jig shown in FIG. 17;

FIG. 19 is a frontal view of a brazing jig with individual support members;

FIG. 20 illustrates an alternate brazing jig with integral alignment means; and

FIG. 21 is a graph of measured sonoluminescence data taken with a sphere fabricated in accordance with the invention.

DESCRIPTION OF THE SPECIFIC EMBODIMENTS

FIG. 1 is an illustration of a spherical sonoluminescence cavitation chamber 101, hereafter referred to as simply a cavitation chamber, fabricated in accordance with the invention. In order to better illustrate the mounting locations of the acoustic transducers in this particular embodiment, FIG. 1 includes centerlines 103-106. Mounted to the exterior surface of cavitation chamber 101 are a total of 6 acoustic transducers, transducers 109-112 mounted to the lower hemisphere of chamber 101 and transducers 115-116 mounted to the upper hemisphere of chamber 101. It will be appreciated that the invention is not limited to a particular number or type of transducer, nor is the invention limited to having transducers mounted to one or more particular locations.

FIG. 2 is a cross-sectional view of a spherical cavitation chamber 201 fabricated in accordance with the invention. Chamber 201 has an outer spherical surface 203 defining the outer diameter of the chamber and an inner spherical surface 205 defining the inner diameter of the chamber.

Chamber 201 can be fabricated from any of a variety of metals although there are some constraints placed on the chamber material. First, the material should be machinable. Second, if the chamber is to be operated at a high temperature, the chamber material should have a relatively high melting temperature. Additionally, a high melting temperature is useful during the fabrication process when the two halves of the chamber are coupled. Third, the chamber material should be corrosion resistant, thus allowing the chamber to be used repeatedly. Fourth, the material should be hard enough to allow a good surface finish to be obtained. In the preferred embodiment of the invention, the chamber is fabricated from 17-4 precipitation hardened stainless steel.

With respect to the dimensions of the chamber, both inner and outer diameters, the selected sizes depend upon the intended use of the chamber. For example, smaller chambers are typically preferable for situations in which it is desirable to limit the amount of cavitating medium, for example due to cost, or the applied energy (e.g., acoustic energy). On the other hand large chambers, on the order of 8-10 inches or greater, typically simplify experimental set-up and event observation. Thick chamber walls are preferable if the chamber is to be operated at high static pressures. Although the invention is not limited to specific dimensions as previously noted, typical wall thicknesses include 0.25 inches, 0.5 inches, 0.75 inches, 1.5 inches, 2.375 inches, 3.5 inches and 4 inches. Typical outside diameters are in the range of 2-10 inches.

The preferred embodiment of the invention provides a means of fabricating spherical chambers while at the same time minimizing wasted material, and thus cost. The first step in the preferred method is to mount a piece 301 of the desired material into jaws 303 of lathe chuck assembly 304. The diameter 305 of piece 301 is preferably only slightly larger than the desired chamber diameter, typically on the order of 0.125 to 0.25 inches greater. Similarly, the length 307 is preferably only slightly larger than one half of the desired chamber diameter.

As illustrated in FIG. 4, the inside spherical surface 401 is then fabricated (i.e., turned) to the desired diameter using the lathe. If desired, a through hole 403 can be bored into piece 301 at this time. Next, without removing piece 301 from the lathe chuck, a portion 501 of the outer spherical surface is turned (FIG. 5). Additionally surface 503 is turned while piece 301 is mounted within chuck assembly 304.

FIGS. 6 and 7 illustrate the preferred jaw assembly used during the next phase of chamber fabrication. FIG. 6 is a cross-sectional view of lathe chuck assembly 601 and FIG. 7 is an end view of chuck assembly 601. Although chuck assembly 601 is shown with 4 jaws 603, it will be appreciated that chuck assembly 601 could have fewer jaws (e.g., a 3 jaw chuck) or more jaws (e.g., a 6 jaw chuck). Holding surfaces 605 of jaws 603 are shaped such that they have a curvature that matches the curvature of surface 501 of piece 301. Curving the surfaces of jaws 603 provides a large contact area between jaws 603 and surface 501, thus spreading out the force applied to the chamber by the jaws. As a result, thinner wall thicknesses can be achieved without deforming the chamber walls, a result that is difficult to achieve using standard, straight-faced jaws. Additionally this approach provides a stronger mounting configuration, thus preventing piece 301 from being pulled out of chuck assembly 601, or moving within chuck assembly 601, during the final fabrication of the outer surface of the spherical chamber. It will be appreciated that if piece 301 moves within the chuck assembly even by a minor amount, the finished chamber half will not have the preferred inside/outside spherical symmetry.

FIG. 8 illustrates piece 301 mounted in chuck assembly 601. During the final step of fabricating this spherical cavitation chamber half, surface 901 is turned as shown in FIG. 9.

Prior to chamber assembly, chamber surface 503 is finished flat. Assuming a chamber outside diameter of 10 inches or less, surface 503 is finished flat to within at least ±0.01 inches, preferably within ±0.001 inches, and still more preferably within ±0.0005 inches. For diameters greater than 10 inches, the inventor has found that as a general rule, the finish surfaces previously noted are multiplied by a tenth of desired chamber's outside diameter (in inches). Thus for example, assuming a desired chamber diameter of 30 inches, the end surface would be finished flat to within at least ±0.03 inches, preferably within ±0.003 inches, and still more preferably within ±0.0015 inches.

Although preferably the spherical chamber halves are fabricated as disclosed above, it will be understood that the inventor also envisions minor variations of this fabrication technique. For example as illustrated in FIG. 10, dimension 307 of a stock piece 1001 can be larger than noted above with respect to FIG. 3. Then during the initial fabrication step (FIG. 11), a cylindrical portion 1003 is turned as well as inside spherical surface 401.

Next, as illustrated in FIG. 12, piece 1001 is removed from chuck assembly 304, reversed, and mounted within chuck assembly 1201. Chuck assembly 1201 may be the same as chuck assembly 304 or may be different, for example having jaws 1203 which have the same curvature as that of cylindrical portion 1003. The outside spherical surface 1301 is then fabricated (i.e., turned) as shown in FIG. 13. If desired, at this point through hole external features (i.e., pipe threads) can be added.

After turning outside surface 1301, the spherical chamber half is removed from cylindrical portion 1003 along line 1303. Assuming a chamber outside diameter of 10 inches or less, the end surface of the chamber half is then finished flat to within at least ±0.01 inches, preferably within ±0.001 inches, and still more preferably within ±0.0005 inches. For diameters greater than 10 inches, the inventor has found that as a general rule, the finish surfaces previously noted are multiplied by a tenth of desired chamber's outside diameter (in inches). Thus for example, assuming a desired chamber diameter of 30 inches, the end surface would be finished flat to within at least ±0.03 inches, preferably within ±0.003 inches, and still more preferably within ±0.0015 inches.

In the preferred embodiment of the invention, the inner and outer spherical chamber surfaces are used as turned. It will be appreciated, however, that various surface finishing procedures (e.g., surface grinding or polishing) can be performed on either or both surfaces if desired.

Regardless of the exact method of fabricating the spherical chamber halves, the next step is to join two halves to form the desired cavitation chamber. As shown in FIG. 14, spherical chamber halves 1401 and 1402 are ready to be joined. As illustrated, chamber half 1401 includes a through hole while chamber half 1402 does not although as previously described, one or both chamber halves can include any number of through holes or ports. Preferably any desired through holes or ports are completed prior to joining the chamber halves, thus insuring that the inner surfaces are finished and cleaned, a process that is more difficult after the chamber halves have been joined.

After the surfaces to be mated, surfaces 1405 and 1407, are finished as previously described, they are ready to be joined, preferably using a brazing operation. The selection of the brazing material depends on the material comprising the half spheres. In the preferred embodiment in which the sphere is comprised of stainless steel, typical brazing materials are comprised of nickel and chromium with small percentages of silicon and boron. Such brazing materials can be obtained, for example, from Vacuum Process Engineering, Inc. in Sacramento, Calif. As numerous suitable brazing materials are well known by those of skill in the brazing industry, further detail is not provided herein.

Brazing material 1403 is preferably formed from a sheet, thus insuring a continuous bond of uniform thickness. As can be seen in FIG. 15, brazing material 1403 is preferably formed as a ring with approximately the same width 1501 as the wall thickness of the sphere. This approach provides a bond of approximately the same width as the sphere walls, yielding a considerably stronger bond then simply bonding/welding around the perimeter of the sphere along the joint line. In the preferred embodiment the thickness of material 803 is in the range of 0.0005 to 0.0025 inches.

During the brazing operation, spherical cavitation chamber halves 1401 and 1402 are pressed together with brazing material 1403 interposed between the half sphere surfaces as shown. The inventor has found that a superior braze is formed by applying force in directions 1601 and 1602 as shown in FIG. 16. Furthermore, preferably the brazing chamber is evacuated prior to heating the chamber halves and the brazing material. Assuming a vacuum brazing process is used as preferred, at least one through hole 403 must be included in at least one of the chamber halves to allow pressure relief/equalization. Typically the brazing temperature is on the order of 100° to 200° F. above the melting temperature of the brazing material. In the preferred embodiment with a 9.5 inch outside diameter sphere of 17-4 stainless steel, the brazing temperature is on the order of 1550° to 1650° F. and the force applied in directions 1601 and 1602 is preferably at least 1000 lbs.

During the joining process, spherical cavitation chamber halves 1401 and 1402 are aligned to insure that the inner sphere surface does not have a discontinuity at the seam line after fabrication. One process for insuring alignment is to use two or more alignment pins 1603 with corresponding holes 1605 as shown in FIG. 16. The inventor has found that if the coefficient of thermal expansion of alignment pins 1603 and the spherical chamber halves differ greatly, alignment issues may arise during the brazing operation. Differences in thermal expansion may also lead to sphere deformation. Accordingly in the preferred embodiment alignment pins 1603 are fabricated from the same material as that of the spherical chamber halves.

Minimizing surface deformation during the brazing operation is critical to insure that the final chamber is a true sphere, a goal which becomes more difficult to obtain as the brazing temperature and/or applied force is increased, and as the chamber wall thickness is decreased. Accordingly a brazing jig 1701 is used in the preferred embodiment of the invention, wherein a first jig half 1703 applies force to chamber half 1401 and a second jig half 1705 applies force to chamber half 1402. In keeping with the goal of minimizing surface deformation, preferably each jig half contacts the corresponding chamber half over a relatively large surface area, thus distributing the applied force. Assuming a vacuum brazing process is used as preferred, preferably jig halves 1703 and 1705 each include a pressure relief through hole 1706.

Assuming a brazing jig is used rather than simply applying force on the two sphere halves, the invention does not require a specific brazing jig configuration. As previously noted, however, it is advantageous to distribute the applied force over as large an area as reasonable. Accordingly in the embodiment illustrated in FIG. 17, sphere contact surfaces 1707 of jig portions 1703 and 1705 are bowl shaped with a curvature that corresponds to the curvature of spherical chamber halves 1401 and 1402, respectively, thus spreading the force over a very large area. In the illustrated embodiment, the central portion 1709 of surfaces 1707 is removed. It will be appreciated that portion 1709 need not be removed, nor is the size of portion 1709 critical as long as sufficient contact surfaces 1707 are provided to distribute the applied force. Preferably surfaces 1707 are continuous, i.e., a ring as illustrated in the frontal view of jig portion 1703 shown in FIG. 18. Note that surface 1707 shown in FIG. 18 has the central portion 1709 removed as illustrated in the cross-sectional of FIG. 17.

In addition to allowing surfaces 1707 to be either a half of a sphere (i.e., bowl shaped) or a spherical ring (i.e., half of a sphere with a central portion 1709 removed), surfaces 1707 can be comprised of individual support members. For example, FIG. 19 illustrates the frontal view of jig portion 1703 in which surface 1707 is divided into four individual support members 1901. Although maximizing surfaces 1707 is preferred from the standpoint of distributing the force applied by the jig halves to the chamber halves, thus minimizing the risk of deformation, it will be appreciated that removing portions of surfaces 1707 allow the addition of external features (e.g., tubes, diagnostics, etc.) to the chamber halves prior to performing the brazing process.

In the preferred embodiment of the invention, a layer 1715 of release material is interposed between surfaces 1707 of brazing jig 1701 and the outer surfaces of chamber halves 1401 and 1402. Layer 1715 is used to aid in the removal of the brazed spherical chamber from jig portions 1703 and 1705 by preventing accidental bonding via diffusion or brazing material drips. Although any of a variety of high temperature metals can be used, in the preferred embodiment in which the spherical chamber is comprised of stainless steel, layer 1715 is comprised of a thin foil of tungsten.

As previously noted, during the brazing operation it is critical to maintain the alignment of the spherical cavitation chamber halves to minimize surface discontinuities at the braze joint. Preferably alignment pins integral to the chamber halves are used as previously described. Alternately the alignment means may be included in the brazing jig. For example as illustrated in FIG. 20, surfaces 1711 and 1713 of jig portions 1703 and 1705, respectively, include multiple alignment pins 2001 and corresponding holes 2003. It will be appreciated that even if the alignment means is integral to the chamber halves as preferred and illustrated in FIGS. 16 and 17, it may be beneficial to include additional alignment means that are integral to the brazing jig.

FIG. 21 is a graph that illustrates the sonoluminescence effect with a sphere fabricated in accordance with the invention. The sphere was fabricated from stainless steel and had an outer diameter of 9.5 inches and an inner diameter of 8 inches. Six acoustic drivers (i.e., transducers) were mounted as illustrated in FIG. 1. For the data shown in FIG. 21, the liquid within the chamber was acetone. During operation, the temperature of the acetone was −27.5° C. The driving frequency was 23.52 kHz, the driving amplitude was 59 V RMS, and the driving power was 8.8 watts. Two acoustic cycles are shown in FIG. 21. It will be appreciated that the data shown in FIG. 21 is only provided for illustration, and that the invention is not limited to this specific configuration.

As will be understood by those familiar with the art, the present invention may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. Accordingly, the disclosures and descriptions herein are intended to be illustrative, but not limiting, of the scope of the invention which is set forth in the following claims. 

1. A method of fabricating a cavitation chamber comprising the steps: a) mounting a piece of stock material in a first lathe chuck; b) finishing a first mating surface of a first half sphere; c) turning an internal spherical surface corresponding to an inside surface of said first half sphere; d) turning a first portion of an external surface of said first half sphere; e) dismounting said piece of stock material and reversing a mounting position of said piece of stock material relative to a first lathe chuck position; f) mounting said piece of stock material in a second lathe chuck; g) turning a second portion of said external surface of said first half sphere; h) repeating steps a) through g) with a second piece of stock material to form a second half sphere, said second half sphere having a second mating surface, both said first and second half spheres having a first inner diameter and a first outer diameter; i) locating a ring-shaped sheet of brazing material between said first and second mating surfaces, said ring-shaped sheet having a second inner diameter approximately equivalent to said first inner diameter, and said ring-shaped sheet having a second outer diameter approximately equivalent to said first outer diameter; and j) brazing said first and second mating surfaces together.
 2. The method of fabricating the cavitation chamber of claim 1, wherein step b) is performed after step d).
 3. The method of fabricating the cavitation chamber of claim 1, wherein step b) is performed after step g).
 4. The method of fabricating the cavitation chamber of claim 1, further comprising the step of boring a through-hole in said first half sphere, wherein said boring step is performed before step e).
 5. The method of fabricating the cavitation chamber of claim 1, further comprising the step of boring a through-hole in said first half sphere, wherein said boring step is performed after step g).
 6. The method of fabricating the cavitation chamber of claim 1, wherein step d) is performed before step c).
 7. The method of fabricating the cavitation chamber of claim 1, wherein said external surface of said first half sphere has a first curvature, and wherein said step of mounting within said second lathe chuck further comprises the step of selecting a second lathe chuck with a plurality of jaws, wherein each jaw of said plurality of jaws has a holding surface with a second curvature matching said first curvature.
 8. The method of fabricating the cavitation chamber of claim 1, wherein said first and second lathe chucks are the same.
 9. The method of fabricating the cavitation chamber of claim 1, wherein said finishing step comprises obtaining a surface flatness of within ±0.01 inches.
 10. The method of fabricating the cavitation chamber of claim 1, wherein said finishing step comprises obtaining a surface flatness of within ±0.001 inches.
 11. The method of fabricating the cavitation chamber of claim 1, wherein said finishing step comprises obtaining a surface flatness of within ±0.0005 inches.
 12. The method of fabricating the cavitation chamber of claim 1, further comprising the step of selecting said piece of stock material from an alloy.
 13. The method of fabricating the cavitation chamber of claim 12, wherein said alloy is a stainless steel alloy.
 14. The method of fabricating the cavitation chamber of claim 1, further comprising the step of maintaining a thickness of said ring-shaped sheet of brazing material of between 0.0005 and 0.0025 inches prior to said brazing step.
 15. The method of fabricating the cavitation chamber of claim 1, said brazing step further comprising the step of evacuating a heating chamber used during said brazing step.
 16. The method of fabricating the cavitation chamber of claim 1, said brazing step further comprising the step of applying compressive force to said first and second half spheres.
 17. The method of fabricating the cavitation chamber of claim 16, wherein said compressive force is at least 1000 lbs.
 18. The method of fabricating the cavitation chamber of claim 1, wherein said brazing step is performed at a temperature of approximately 100° to 200° F. above a melting temperature of said brazing material.
 19. The method of fabricating the cavitation chamber of claim 1, further comprising the steps: k) mounting at least one alignment pin in said first mating surface; l) boring at least one hole corresponding to said at least one alignment pin in said second mating surface; and m) aligning said at least one alignment pin and said at least one corresponding hole prior to said brazing step j).
 20. The method of fabricating the cavitation chamber of claim 1, further comprising the step of positioning said first and second half spheres in a brazing jig prior to performing said brazing step j).
 21. A method of fabricating a cavitation chamber comprising the steps: a) mounting a piece of stock material in a lathe chuck; b) turning an internal spherical surface corresponding to an inside surface of a first half sphere; c) forming a cylindrical end portion on said piece of stock material; d) dismounting said piece of stock material and reversing a mounting position of said piece of stock material relative to said lathe chuck; e) remounting said piece of stock material into said lathe chuck; f) turning an external spherical surface corresponding to an outside surface of said first half sphere; g) removing excess stock material from said first half sphere; h) finishing a first mating surface of said first half sphere; i) repeating steps a) through h) with a second piece of stock material to form a second half sphere, said second half sphere having a second mating surface, both said first and second half spheres having a first inner diameter and a first outer diameter; j) locating a ring-shaped sheet of brazing material between said first and second mating surfaces, said ring-shaped sheet having a second inner diameter approximately equivalent to said first inner diameter, and said ring-shaped sheet having a second outer diameter approximately equivalent to said first outer diameter; and k) brazing said first and second mating surfaces together.
 22. The method of fabricating the cavitation chamber of claim 21, wherein step c) is performed before step b).
 23. The method of fabricating the cavitation chamber of claim 21, further comprising the step of boring a through-hole in said first half sphere, wherein said boring step is performed before step d).
 24. The method of fabricating the cavitation chamber of claim 21, further comprising the step of boring a through-hole in said first half sphere, wherein said boring step is performed before step i).
 25. The method of fabricating the cavitation chamber of claim 21, wherein said finishing step comprises obtaining a surface flatness of within ±0.01 inches.
 26. The method of fabricating the cavitation chamber of claim 21, wherein said finishing step comprises obtaining a surface flatness of within ±0.001 inches.
 27. The method of fabricating the cavitation chamber of claim 21, wherein said finishing step comprises obtaining a surface flatness of within ±0.0005 inches.
 28. The method of fabricating the cavitation chamber of claim 21, further comprising the step of selecting said piece of stock material from an alloy.
 29. The method of fabricating the cavitation chamber of claim 28, wherein said alloy is a stainless steel alloy.
 30. The method of fabricating the cavitation chamber of claim 21, further comprising the step of maintaining a thickness of said ring-shaped sheet of brazing material of between 0.0005 and 0.0025 inches prior to said brazing step.
 31. The method of fabricating the cavitation chamber of claim 21, said brazing step further comprising the step of evacuating a heating chamber used during said brazing step.
 32. The method of fabricating the cavitation chamber of claim 21, said brazing step further comprising the step of applying compressive force to said first and second half spheres.
 33. The method of fabricating the cavitation chamber of claim 32, wherein said compressive force is at least 1000 lbs.
 34. The method of fabricating the cavitation chamber of claim 21, wherein said brazing step is performed at a temperature of approximately 100° to 200° F. above a melting temperature of said brazing material.
 35. The method of fabricating the cavitation chamber of claim 21, further comprising the steps: l) mounting at least one alignment pin in said first mating surface; m) boring at least one hole corresponding to said at least one alignment pin in said second mating surface; and n) aligning said at least one alignment pin and said at least one corresponding hole prior to said brazing step j).
 36. The method of fabricating the cavitation chamber of claim 21, further comprising the step of positioning said first and second half spheres in an alignment jig prior to performing said brazing step k).
 37. A method of fabricating a cavitation system comprising the steps: a) mounting a piece of stock material in a first lathe chuck; b) finishing a first mating surface of a first spherical cavitation chamber half; c) turning an internal spherical surface corresponding to an inside surface of said first spherical cavitation chamber half; d) turning a first portion of an external surface of said first spherical cavitation chamber half, wherein said external surface of said first spherical cavitation chamber half has a first curvature; e) dismounting said piece of stock material and reversing a mounting position of said piece of stock material relative to a first lathe chuck position; f) mounting said piece of stock material in a second lathe chuck, wherein said second lathe chuck has a plurality of jaws, wherein each jaw of said plurality of jaws has a holding surface with a second curvature matching said first curvature; g) turning a second portion of said external surface of said first spherical cavitation chamber half; h) repeating steps a) through g) with a second piece of stock material to form a second spherical cavitation chamber half, said second spherical cavitation chamber half having a second mating surface, both said first and second spherical cavitation chamber halves having a first inner diameter and a first outer diameter; i) locating a ring-shaped sheet of brazing material between said first and second mating surfaces, said ring-shaped sheet having a second inner diameter approximately equivalent to said first inner diameter, and said ring-shaped sheet having a second outer diameter approximately equivalent to said first outer diameter; j) aligning said first and second spherical cavitation chamber halves; and k) brazing said first and second mating surfaces together; and l) coupling at least one acoustic transducer to said external spherical surface.
 38. The method of fabricating the cavitation chamber of claim 37, wherein step b) is performed after step d).
 39. The method of fabricating the cavitation chamber of claim 37, wherein step b) is performed after step g).
 40. The method of fabricating the cavitation chamber of claim 37, further comprising the step of boring a through-hole in said first spherical cavitation chamber half, wherein said boring step is performed before step e).
 41. The method of fabricating the cavitation chamber of claim 37, further comprising the step of boring a through-hole in said first spherical cavitation chamber half, wherein said boring step is performed after step g).
 42. The method of fabricating the cavitation chamber of claim 37, wherein step d) is performed before step c).
 43. The method of fabricating the cavitation system of claim 37, wherein said finishing step comprises obtaining a surface flatness of at least ±0.01 inches.
 44. The method of fabricating the cavitation system of claim 37, further comprising the step of selecting said piece of stock material from an alloy.
 45. The method of fabricating the cavitation system of claim 44, wherein said alloy is a stainless steel alloy.
 46. The method of fabricating the cavitation system of claim 37, further comprising the step of maintaining a thickness of said ring-shaped sheet of brazing material of between 0.0005 and 0.0025 inches prior to said brazing step.
 47. The method of fabricating the cavitation system of claim 37, said brazing step further comprising the step of evacuating a heating chamber used during said brazing step.
 48. The method of fabricating the cavitation system of claim 37, said brazing step further comprising the step of applying compressive force to said first and second spherical cavitation chamber halves.
 49. The method of fabricating the cavitation system of claim 37, wherein said brazing step is performed at a temperature of approximately 100° to 200° F. above a melting temperature of said brazing material.
 50. The method of fabricating the cavitation system of claim 37, said aligning step further comprising the steps: m) mounting at least one alignment pin in said first mating surface; n) boring at least one hole corresponding to said at least one alignment pin in said second mating surface; and o) aligning said at least one alignment pin and said at least one corresponding hole prior to said brazing step k).
 51. The method of fabricating the cavitation system of claim 37, said aligning step further comprising the step of positioning said first and second spherical cavitation chamber halves in a brazing jig prior to performing said brazing step k).
 52. A method of fabricating a cavitation system comprising the steps: a) mounting a piece of stock material in a lathe chuck; b) turning an internal spherical surface corresponding to an inside surface of a first spherical cavitation chamber half; c) forming a cylindrical end portion on said piece of stock material; d) dismounting said piece of stock material and reversing a mounting position of said piece of stock material relative to said lathe chuck; e) remounting said piece of stock material into said lathe chuck; f) turning an external spherical surface corresponding to an outside surface of said first spherical cavitation chamber half; g) removing excess stock material from said first spherical cavitation chamber half; h) finishing a first mating surface of said first spherical cavitation chamber half; i) repeating steps a) through h) with a second piece of stock material to form a second spherical cavitation chamber half, said second spherical cavitation chamber half having a second mating surface, both said first and second spherical cavitation chamber halves having a first inner diameter and a first outer diameter; j) locating a ring-shaped sheet of brazing material between said first and second mating surfaces, said ring-shaped sheet having a second inner diameter approximately equivalent to said first inner diameter, and said ring-shaped sheet having a second outer diameter approximately equivalent to said first outer diameter; k) aligning said first and second spherical cavitation chamber halves; l) brazing said first and second mating surfaces together; and m) coupling at least one acoustic transducer to said external spherical surface.
 53. The method of fabricating the cavitation chamber of claim 52, wherein step c) is performed before step b).
 54. The method of fabricating the cavitation chamber of claim 52, further comprising the step of boring a through-hole in said first spherical cavitation chamber half, wherein said boring step is performed before step d).
 55. The method of fabricating the cavitation chamber of claim 52, further comprising the step of boring a through-hole in said first spherical cavitation chamber half, wherein said boring step is performed before step i).
 56. The method of fabricating the cavitation system of claim 52, wherein said finishing step comprises obtaining a surface flatness of at least ±0.01 inches.
 57. The method of fabricating the cavitation system of claim 52, further comprising the step of selecting said piece of stock material from an alloy.
 58. The method of fabricating the cavitation system of claim 57, wherein said alloy is a stainless steel alloy.
 59. The method of fabricating the cavitation system of claim 52, further comprising the step of maintaining a thickness of said ring-shaped sheet of brazing material of between 0.0005 and 0.0025 inches prior to said brazing step.
 60. The method of fabricating the cavitation system of claim 52, said brazing step further comprising the step of evacuating a heating chamber used during said brazing step.
 61. The method of fabricating the cavitation system of claim 52, said brazing step further comprising the step of applying compressive force to said first and second spherical cavitation chamber halves.
 62. The method of fabricating the cavitation system of claim 52, wherein said brazing step is performed at a temperature of approximately 100° to 200° F. above a melting temperature of said brazing material.
 63. The method of fabricating the cavitation system of claim 52, said aligning step further comprising the steps of: n) mounting at least one alignment pin in said first mating surface; o) boring at least one hole corresponding to said at least one alignment pin in said second mating surface; and p) aligning said at least one alignment pin and said at least one corresponding hole.
 64. The method of fabricating the cavitation system of claim 52, said aligning step further comprising the step of positioning said first and second spherical cavitation chamber halves in an alignment jig. 